[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19116 7 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2741800
64 A = 6794074
34 meter
Y = 4817789
38 meter E =
0019595
Z = 3911428
56 I = 52
00200
XDOT = -3580
671355 Wp = 90
37696
YDOT = -5392
944828 meter/sec RA = 86
19186 deg
ZDOT = 4114
782804 TA = 316
64479
MA = 316
79878
Ha = 230
276 n
mi
Hp = 217
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8995408
93 X = -2814471
24
Y = 15806395
59 feet Y = 4786721
89 meter
Z = 12832770
85 Z = 3897933
28
XDOT = -11747
609432 XDOT = -3540
088813
YDOT = -17693
388542 feet/sec YDOT = -5432
759896 meter/sec
ZDOT = 13499
943583 ZDOT = 4097
485803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15651900
43 X = 4770699
25
Y = 9340316
61 feet Y = 2846928
50 meter
Z = 12775602
91 Z = 3894003
77
XDOT = -17208
495137 XDOT = -5245
149318
YDOT = 10389
119160 feet/sec YDOT = 3166
603520 meter/sec
ZDOT = 13428
370161 ZDOT = 4092
967225
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13172
55605162
00016717 00000-0 10270-3 0 9001
2 25544 51
6491 86
6868 0008691 79
5811 280
6319 15
50298619 35389
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55605162 = yrday
fracday
Element set: 900
Inclination: 51
6491 deg
RA of node: 86
6868 deg
Eccentricity:
0008691
Arg of perigee: 79
5811 deg
Mean anomaly: 280
6319 deg
Mean motion: 15
50298619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 334
Coasting Arc #2 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2013/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2628229
90 A = 6792905
40 meter
Y = -4637931
22 meter E =
0016439
Z = -4226532
08 I = 51
99670
XDOT = 3781
657963 Wp = 76
63373
YDOT = 5516
748336 meter/sec RA = 81
25902 deg
ZDOT = -3710
580352 TA = 155
40605
MA = 155
32756
Ha = 230
131 n
mi
Hp = 217
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8622801
49 X = 2700428
31
Y = -15216309
76 feet Y = -4608136
27 meter
Z = -13866575
06 Z = -4213589
77
XDOT = 12407
014313 XDOT = 3737
712470
YDOT = 18099
568032 feet/sec YDOT = 5558
792153 meter/sec
ZDOT = -12173
820052 ZDOT = -3692
315127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15220133
55 X = -4639096
71
Y = -8703691
82 feet Y = -2652885
27 meter
Z = -13811733
26 Z = -4209816
30
XDOT = 17460
010410 XDOT = 5321
811173
YDOT = -11377
941289 feet/sec YDOT = -3467
996505 meter/sec
ZDOT = -12098
218937 ZDOT = -3687
537132
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13173
52295655
00016717 00000-0 10270-3 0 9012
2 25544 51
6503 81
8947 0008643 82
6932 277
5201 15
50340615 35530
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
52295655 = yrday
fracday
Element set: 901
Inclination: 51
6503 deg
RA of node: 81
8947 deg
Eccentricity:
0008643
Arg of perigee: 82
6932 deg
Mean anomaly: 277
5201 deg
Mean motion: 15
50340615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 306
Coasting Arc #3 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2013/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2511632
59 A = 6791964
63 meter
Y = 4444513
99 meter E =
0017386
Z = 4466522
79 I = 51
98786
XDOT = -4032
611048 Wp = 98
85121
YDOT = -5621
625843 meter/sec RA = 76
32539 deg
ZDOT = 3312
716025 TA = 317
84244
MA = 317
97602
Ha = 230
196 n
mi
Hp = 217
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8240264
39 X = -2582842
51
Y = 14581738
80 feet Y = 4416028
38 meter
Z = 14653946
17 Z = 4454149
37
XDOT = -13230
351206 XDOT = -3985
541315
YDOT = -18443
654340 feet/sec YDOT = -5666
458444 meter/sec
ZDOT = 10868
490897 ZDOT = 3293
239373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14726571
54 X = 4488659
01
Y = 8074121
04 feet Y = 2460992
09 meter
Z = 14601502
05 Z = 4450537
83
XDOT = -17618
292702 XDOT = -5370
055616
YDOT = 12544
488384 feet/sec YDOT = 3823
560059 meter/sec
ZDOT = 10787
838962 ZDOT = 3288
133316
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13174
55430776
00016717 00000-0 10270-3 0 9022
2 25544 51
6501 76
7834 0008618 86
6040 273
6096 15
50346236 35693
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
55430776 = yrday
fracday
Element set: 902
Inclination: 51
6501 deg
RA of node: 76
7834 deg
Eccentricity:
0008618
Arg of perigee: 86
6040 deg
Mean anomaly: 273
6096 deg
Mean motion: 15
50346236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 319
Coasting Arc #4 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2013/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476658
05 A = 6790901
55 meter
Y = -4222036
55 meter E =
0018978
Z = -4724872
96 I = 51
97710
XDOT = 4260
159626 Wp = 78
84423
YDOT = 5677
442097 meter/sec RA = 71
38999 deg
ZDOT = -2846
286185 TA = 162
99355
MA = 162
92986
Ha = 230
013 n
mi
Hp = 217
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8125518
53 X = 2546637
64
Y = -13851825
97 feet Y = -4193948
95 meter
Z = -15501551
70 Z = -4712672
40
XDOT = 13976
901661 XDOT = 4210
182973
YDOT = 18626
778534 feet/sec YDOT = 5724
802921 meter/sec
ZDOT = -9338
209267 ZDOT = -2825
711363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14130070
79 X = -4306845
58
Y = -7735521
31 feet Y = -2357786
90 meter
Z = -15449855
94 Z = -4709116
09
XDOT = 17563
587117 XDOT = 5353
381353
YDOT = -13642
141336 feet/sec YDOT = -4158
124679 meter/sec
ZDOT = -9252
970873 ZDOT = -2820
305522
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13175
52118462
00016717 00000-0 10270-3 0 9036
2 25544 51
6507 71
9911 0008508 89
5843 270
6283 15
50387797 35842
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
52118462 = yrday
fracday
Element set: 903
Inclination: 51
6507 deg
RA of node: 71
9911 deg
Eccentricity:
0008508
Arg of perigee: 89
5843 deg
Mean anomaly: 270
6283 deg
Mean motion: 15
50387797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 332
Coasting Arc #5 (Orbit 3599)
---------------------------------------
Vector Time (GMT): 2013/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446444
67 A = 6790081
79 meter
Y = 3993118
26 meter E =
0014855
Z = 4905941
43 I = 51
96349
XDOT = -4526
048862 Wp = 105
43351
YDOT = -5715
398545 meter/sec RA = 66
45329 deg
ZDOT = 2385
113572 TA = 321
26087
MA = 321
36730
Ha = 230
087 n
mi
Hp = 217
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8026393
27 X = -2514746
18
Y = 13100781
69 feet Y = 3965377
98 meter
Z = 16095608
36 Z = 4893891
64
XDOT = -14849
241674 XDOT = -4473
387741
YDOT = -18751
307561 feet/sec YDOT = -5765
717574 meter/sec
ZDOT = 7825
175762 ZDOT = 2363
253808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13506100
80 X = 4116659
52
Y = 7434985
86 feet Y = 2266183
69 meter
Z = 16044572
43 Z = 4890385
68
XDOT = -17410
130561 XDOT = -5306
607795
YDOT = 14865
556948 feet/sec YDOT = 4531
021758 meter/sec
ZDOT = 7734
565955 ZDOT = 2357
495703
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13176
55250609
00016717 00000-0 10270-3 0 9041
2 25544 51
6504 66
8792 0008504 93
5350 266
6774 15
50393572 36000
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
55250609 = yrday
fracday
Element set: 904
Inclination: 51
6504 deg
RA of node: 66
8792 deg
Eccentricity:
0008504
Arg of perigee: 93
5350 deg
Mean anomaly: 266
6774 deg
Mean motion: 15
50393572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3600
Checksum: 315
Coasting Arc #6 (Orbit 3614)
---------------------------------------
Vector Time (GMT): 2013/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2499616
38 A = 6789255
05 meter
Y = -3753557
34 meter E =
0021119
Z = -5093858
92 I = 51
94791
XDOT = 4751
757854 Wp = 83
85391
YDOT = 5692
320162 meter/sec RA = 61
51431 deg
ZDOT = -1867
262167 TA = 168
10498
MA = 168
05503
Ha = 229
871 n
mi
Hp = 217
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8200841
13 X = 2566147
95
Y = -12314820
67 feet Y = -3725232
45 meter
Z = -16712135
57 Z = -5081555
01
XDOT = 15589
756738 XDOT = 4696
822470
YDOT = 18675
591084 feet/sec YDOT = 5745
150378 meter/sec
ZDOT = -6126
188211 ZDOT = -1844
311620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12860268
02 X = -3919809
69
Y = -7433686
08 feet Y = -2265787
52 meter
Z = -16660068
92 Z = -5077989
01
XDOT = 17009
101757 XDOT = 5184
374216
YDOT = -15942
130572 feet/sec YDOT = -4859
161398 meter/sec
ZDOT = -6031
011324 ZDOT = -1838
252251
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13177
51935513
00016717 00000-0 10270-3 0 9053
2 25544 51
6503 62
0863 0008341 96
4764 263
7337 15
50433926 36153
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
51935513 = yrday
fracday
Element set: 905
Inclination: 51
6503 deg
RA of node: 62
0863 deg
Eccentricity:
0008341
Arg of perigee: 96
4764 deg
Mean anomaly: 263
7337 deg
Mean motion: 15
50433926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3615
Checksum: 310
Coasting Arc #7 (Orbit 3630)
---------------------------------------
Vector Time (GMT): 2013/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2561878
14 A = 6788679
67 meter
Y = 3515646
53 meter E =
0012385
Z = 5202460
78 I = 51
93064
XDOT = -5002
186414 Wp = 108
26808
YDOT = -5655
897758 meter/sec RA = 56
57425 deg
ZDOT = 1352
391274 TA = 328
75419
MA = 328
82774
Ha = 229
948 n
mi
Hp = 217
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8405112
01 X = -2626272
31
Y = 11534273
41 feet Y = 3486637
44 meter
Z = 17068440
89 Z = 5189859
49
XDOT = -16411
372750 XDOT = -4945
138642
YDOT = -18556
095007 feet/sec YDOT = -5711
516526 meter/sec
ZDOT = 4436
979245 ZDOT = 1328
229393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12226421
11 X = 3726613
16
Y = 7484375
87 feet Y = 2281237
77 meter
Z = 17015163
53 Z = 5186221
84
XDOT = -16523
599163 XDOT = -5036
393025
YDOT = 17085
588174 feet/sec YDOT = 5207
687276 meter/sec
ZDOT = 4336
731099 ZDOT = 1321
835639
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13178
55064720
00016717 00000-0 10270-3 0 9062
2 25544 51
6503 56
9741 0008348 100
4688 259
7404 15
50439978 36319
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
55064720 = yrday
fracday
Element set: 906
Inclination: 51
6503 deg
RA of node: 56
9741 deg
Eccentricity:
0008348
Arg of perigee: 100
4688 deg
Mean anomaly: 259
7404 deg
Mean motion: 15
50439978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3631
Checksum: 325
Coasting Arc #8 (Orbit 3645)
---------------------------------------
Vector Time (GMT): 2013/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2703107
34 A = 6788207
20 meter
Y = -3287521
62 meter E =
0022418
Z = -5307522
88 I = 51
91123
XDOT = 5194
270299 Wp = 90
75231
YDOT = 5553
634341 meter/sec RA = 51
63148 deg
ZDOT = -797
735153 TA = 171
64861
MA = 171
61124
Ha = 229
718 n
mi
Hp = 217
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8868462
41 X = 2765450
50
Y = -10785832
08 feet Y = -3256944
73 meter
Z = -17413132
79 Z = -5294240
39
XDOT = 17041
569223 XDOT = 5135
657455
YDOT = 18220
585107 feet/sec YDOT = 5611
392297 meter/sec
ZDOT = -2617
241315 ZDOT = -772
643962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11657048
16 X = -3553068
28
Y = -7813287
57 feet Y = -2381490
05 meter
Z = -17357037
72 Z = -5290425
10
XDOT = 15790
326968 XDOT = 4812
891660
YDOT = -17999
009322 feet/sec YDOT = -5486
098041 meter/sec
ZDOT = -2513
094807 ZDOT = -765
991297
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13179
51746907
00016717 00000-0 10270-3 0 9074
2 25544 51
6499 52
1806 0008173 103
5240 256
6822 15
50477018 36460
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
51746907 = yrday
fracday
Element set: 907
Inclination: 51
6499 deg
RA of node: 52
1806 deg
Eccentricity:
0008173
Arg of perigee: 103
5240 deg
Mean anomaly: 256
6822 deg
Mean motion: 15
50477018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3646
Checksum: 318
Coasting Arc #9 (Orbit 3661)
---------------------------------------
Vector Time (GMT): 2013/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2853707
92 A = 6787980
25 meter
Y = 3068820
51 meter E =
0010618
Z = 5331245
11 I = 51
89115
XDOT = -5396
412964 Wp = 105
33652
YDOT = -5446
105458 meter/sec RA = 46
68830 deg
ZDOT = 243
206248 TA = 342
33568
MA = 342
37257
Ha = 229
786 n
mi
Hp = 217
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9362558
79 X = -2913709
64
Y = 10068308
75 feet Y = 3036572
61 meter
Z = 17490961
65 Z = 5317236
64
XDOT = -17704
766943 XDOT = -5336
293784
YDOT = -17867
800058 feet/sec YDOT = -5506
115431 meter/sec
ZDOT = 797
920762 ZDOT = 217
136674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11136991
87 X = 3394555
12
Y = 8189001
45 feet Y = 2496007
64 meter
Z = 17431860
34 Z = 5313231
03
XDOT = -15007
690281 XDOT = -4574
343998
YDOT = 18920
262207 feet/sec YDOT = 5766
895921 meter/sec
ZDOT = 689
671953 ZDOT = 210
212011
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13180
54873221
00016717 00000-0 10270-3 0 9080
2 25544 51
6502 47
0685 0008163 107
5591 252
6452 15
50485222 36624
Satellite: ISS
Catalog Number: 25544
Epoch time: 13180
54873221 = yrday
fracday
Element set: 908
Inclination: 51
6502 deg
RA of node: 47
0685 deg
Eccentricity:
0008163
Arg of perigee: 107
5591 deg
Mean anomaly: 252
6452 deg
Mean motion: 15
50485222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3662
Checksum: 298
Coasting Arc #10 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2013/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3072337
87 A = 6787944
21 meter
Y = -2879919
63 meter E =
0022556
Z = -5343226
94 I = 51
86866
XDOT = 5523
763497 Wp = 98
79630
YDOT = 5276
154990 meter/sec RA = 41
74195 deg
ZDOT = 330
215550 TA = 174
36389
MA = 174
33846
Ha = 229
565 n
mi
Hp = 217
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10079848
64 X = 3130269
29
Y = -9448555
21 feet Y = -2845238
43 meter
Z = -17530272
11 Z = -5328161
37
XDOT = 18122
583651 XDOT = 5462
749756
YDOT = 17310
219783 feet/sec YDOT = 5337
584026 meter/sec
ZDOT = 1083
384349 ZDOT = 356
901696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10760997
56 X = -3279952
06
Y = -8792138
61 feet Y = -2679843
85 meter
Z = -17466774
59 Z = -5323872
90
XDOT = 14013
993916 XDOT = 4271
465346
YDOT = -19538
842175 feet/sec YDOT = -5955
439095 meter/sec
ZDOT = 1194
229869 ZDOT = 364
001264
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13181
51552756
00016717 00000-0 10270-3 0 9096
2 25544 51
6494 42
2746 0008033 110
8260 249
3752 15
50516162 36775
Satellite: ISS
Catalog Number: 25544
Epoch time: 13181
51552756 = yrday
fracday
Element set: 909
Inclination: 51
6494 deg
RA of node: 42
2746 deg
Eccentricity:
0008033
Arg of perigee: 110
8260 deg
Mean anomaly: 249
3752 deg
Mean motion: 15
50516162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 305
Coasting Arc #11 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2013/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3296408
72 A = 6788130
62 meter
Y = 2706405
89 meter E =
0010335
Z = 5271866
85 I = 51
84631
XDOT = -5646
577971 Wp = 98
13345
YDOT = -5112
430214 meter/sec RA = 36
79572 deg
ZDOT = -906
062941 TA =
50612
MA =
50507
Ha = 229
609 n
mi
Hp = 217
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10814989
22 X = -3352036
62
Y = 8879284
43 feet Y = 2669231
82 meter
Z = 17296151
07 Z = 5255718
34
XDOT = -18525
518279 XDOT = -5584
588596
YDOT = -16773
065008 feet/sec YDOT = -5175
227124 meter/sec
ZDOT = -2972
647443 ZDOT = -933
343435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10461553
48 X = 3188681
50
Y = 9418565
31 feet Y = 2870778
71 meter
Z = 17228147
09 Z = 5251139
23
XDOT = -13025
547581 XDOT = -3970
186903
YDOT = 20113
313549 feet/sec YDOT = 6130
537970 meter/sec
ZDOT = -3085
995721 ZDOT = -940
611496
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13182
54676207
00016717 00000-0 10270-3 0 9100
2 25544 51
6497 37
1626 0007977 114
9083 245
2897 15
50528778 36931
Satellite: ISS
Catalog Number: 25544
Epoch time: 13182
54676207 = yrday
fracday
Element set: 910
Inclination: 51
6497 deg
RA of node: 37
1626 deg
Eccentricity:
0007977
Arg of perigee: 114
9083 deg
Mean anomaly: 245
2897 deg
Mean motion: 15
50528778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 345
Coasting Arc #12 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2013/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3571673
24 A = 6788551
27 meter
Y = -2579716
16 meter E =
0021377
Z = -5183590
15 I = 51
82145
XDOT = 5683
121170 Wp = 107
26538
YDOT = 4897
546115 meter/sec RA = 31
84604 deg
ZDOT = 1477
370230 TA = 176
96965
MA = 176
95668
Ha = 229
413 n
mi
Hp = 217
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11718088
05 X = 3625435
21
Y = -8463635
69 feet Y = -2539474
27 meter
Z = -17006529
35 Z = -5166108
98
XDOT = 18645
410662 XDOT = 5620
756699
YDOT = 16068
064681 feet/sec YDOT = 4960
749499 meter/sec
ZDOT = 4847
015191 ZDOT = 1504
827403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10367062
52 X = -3159880
65
Y = -10196441
04 feet Y = -3107875
23 meter
Z = -16932966
73 Z = -5161168
26
XDOT = 11894
717376 XDOT = 3625
509856
YDOT = -20338
792683 feet/sec YDOT = -6199
264010 meter/sec
ZDOT = 4961
127664 ZDOT = 1512
151712
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13183
51353121
00016717 00000-0 10270-3 0 9116
2 25544 51
6485 32
3683 0007937 118
3325 241
8628 15
50552760 37080
Satellite: ISS
Catalog Number: 25544
Epoch time: 13183
51353121 = yrday
fracday
Element set: 911
Inclination: 51
6485 deg
RA of node: 32
3683 deg
Eccentricity:
0007937
Arg of perigee: 118
3325 deg
Mean anomaly: 241
8628 deg
Mean motion: 15
50552760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 300
Coasting Arc #13 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2013/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3844595
27 A = 6789161
97 meter
Y = 2471047
59 meter E =
0011765
Z = 5010151
97 I = 51
79741
XDOT = -5701
851963 Wp = 93
73544
YDOT = -4703
325343 meter/sec RA = 26
89666 deg
ZDOT = -2052
258945 TA = 16
18758
MA = 16
15003
Ha = 229
429 n
mi
Hp = 217
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12613501
53 X = -3896279
26
Y = 8107111
50 feet Y = 2427765
28 meter
Z = 16437506
47 Z = 4991350
05
XDOT = -18706
863396 XDOT = -5638
865272
YDOT = -15430
857425 feet/sec YDOT = -4766
734615 meter/sec
ZDOT = -6733
133022 ZDOT = -2079
805622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10358773
82 X = 3157354
26
Y = 10959689
28 feet Y = 3340513
29 meter
Z = 16358432
45 Z = 4986050
21
XDOT = -10839
306854 XDOT = -3303
820729
YDOT = 20482
523430 feet/sec YDOT = 6243
073142 meter/sec
ZDOT = -6847
643501 ZDOT = -2087
161739
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13184
54473716
00016717 00000-0 10270-3 0 9124
2 25544 51
6487 27
2561 0007832 122
4671 237
7238 15
50569881 37245
Satellite: ISS
Catalog Number: 25544
Epoch time: 13184
54473716 = yrday
fracday
Element set: 912
Inclination: 51
6487 deg
RA of node: 27
2561 deg
Eccentricity:
0007832
Arg of perigee: 122
4671 deg
Mean anomaly: 237
7238 deg
Mean motion: 15
50569881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 323
Coasting Arc #14 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2013/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147489
96 A = 6789980
73 meter
Y = -2421020
69 meter E =
0018931
Z = -4818251
47 I = 51
77106
XDOT = 5630
639612 Wp = 115
22818
YDOT = 4475
172685 meter/sec RA = 21
94395 deg
ZDOT = 2598
291538 TA = 180
39855
MA = 180
40007
Ha = 229
266 n
mi
Hp = 217
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13607250
53 X = 4197659
79
Y = -7942981
26 feet Y = -2374359
66 meter
Z = -15807911
64 Z = -4797981
85
XDOT = 18473
227075 XDOT = 5567
557014
YDOT = 14682
325081 feet/sec YDOT = 4537
784982 meter/sec
ZDOT = 8524
578538 ZDOT = 2625
492007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10588264
26 X = -3227302
95
Y = -11782342
08 feet Y = -3591257
87 meter
Z = -15722702
17 Z = -4792279
62
XDOT = 9730
058509 XDOT = 2965
721834
YDOT = -20269
703399 feet/sec YDOT = -6178
205596 meter/sec
ZDOT = 8637
671524 ZDOT = 2632
762281
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13185
51148003
00016717 00000-0 10270-3 0 9131
2 25544 51
6473 22
4615 0007899 125
8679 234
3206 15
50589725 37398
Satellite: ISS
Catalog Number: 25544
Epoch time: 13185
51148003 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 22
4615 deg
Eccentricity:
0007899
Arg of perigee: 125
8679 deg
Mean anomaly: 234
3206 deg
Mean motion: 15
50589725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 323
Coasting Arc #15 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2013/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921737
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437339
73 A = 6790959
39 meter
Y = 2386960
94 meter E =
0014282
Z = 4539891
86 I = 51
74591
XDOT = -5531
021374 Wp = 96
11875
YDOT = -4284
229786 meter/sec RA = 16
99149 deg
ZDOT = -3146
527637 TA = 25
40517
MA = 25
33502
Ha = 229
256 n
mi
Hp = 217
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14558201
21 X = -4485754
90
Y = 7831236
67 feet Y = 2337068
45 meter
Z = 14894658
34 Z = 4518218
51
XDOT = -18146
395583 XDOT = -5467
418209
YDOT = -14055
872001 feet/sec YDOT = -4345
725084 meter/sec
ZDOT = -10323
253403 ZDOT = -3173
242836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10890269
29 X = 3319354
08
Y = 12544976
03 feet Y = 3823708
69 meter
Z = 14803578
91 Z = 4512130
85
XDOT = -8775
316090 XDOT = -2674
716344
YDOT = 19958
098242 feet/sec YDOT = 6083
228344 meter/sec
ZDOT = -10434
343210 ZDOT = -3180
387811
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13186
54265734
00016717 00000-0 10270-3 0 9147
2 25544 51
6475 17
3488 0007768 130
0448 230
1386 15
50608490 37550
Satellite: ISS
Catalog Number: 25544
Epoch time: 13186
54265734 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 17
3488 deg
Eccentricity:
0007768
Arg of perigee: 130
0448 deg
Mean anomaly: 230
1386 deg
Mean motion: 15
50608490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 321
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